FR2345591A1 - Disque tournant redondant - Google Patents

Disque tournant redondant

Info

Publication number
FR2345591A1
FR2345591A1 FR7708375A FR7708375A FR2345591A1 FR 2345591 A1 FR2345591 A1 FR 2345591A1 FR 7708375 A FR7708375 A FR 7708375A FR 7708375 A FR7708375 A FR 7708375A FR 2345591 A1 FR2345591 A1 FR 2345591A1
Authority
FR
France
Prior art keywords
rotating disc
redundant
redundant rotating
disc
rotating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Withdrawn
Application number
FR7708375A
Other languages
English (en)
Inventor
William Nickolas Barack
Charles Houston Gay Jr
Stephen William Beckman
Paul Allen Domas
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by General Electric Co filed Critical General Electric Co
Publication of FR2345591A1 publication Critical patent/FR2345591A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/021—Blade-carrying members, e.g. rotors for flow machines or engines with only one axial stage
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49321—Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49826—Assembling or joining
    • Y10T29/49893—Peripheral joining of opposed mirror image parts to form a hollow body

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR7708375A 1976-03-22 1977-03-21 Disque tournant redondant Withdrawn FR2345591A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/668,971 US4097194A (en) 1976-03-22 1976-03-22 Redundant disc

Publications (1)

Publication Number Publication Date
FR2345591A1 true FR2345591A1 (fr) 1977-10-21

Family

ID=24684498

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7708375A Withdrawn FR2345591A1 (fr) 1976-03-22 1977-03-21 Disque tournant redondant

Country Status (5)

Country Link
US (1) US4097194A (fr)
JP (1) JPS52129812A (fr)
CA (1) CA1045041A (fr)
DE (1) DE2712115A1 (fr)
FR (1) FR2345591A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0521614A2 (fr) * 1991-06-06 1993-01-07 General Electric Company Assemblage de disques multiples de rotor

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4787821A (en) * 1987-04-10 1988-11-29 Allied Signal Inc. Dual alloy rotor
US4898514A (en) * 1987-10-27 1990-02-06 United Technologies Corporation Turbine balance arrangement with integral air passage
US5135354A (en) * 1990-09-14 1992-08-04 United Technologies Corporation Gas turbine blade and disk
US5213475A (en) * 1991-12-05 1993-05-25 General Electric Company Burst resistant rotor disk assembly
DE102009004926A1 (de) * 2009-01-16 2010-07-22 Mtu Aero Engines Gmbh Schaufelintegrierte geteilte Scheibe einer Turbinen- oder Verdichterstufe
FR3077327B1 (fr) * 2018-01-30 2020-02-21 Safran Aircraft Engines Ensemble pour turbine de turbomachine comprenant un anneau mobile d'etancheite
US10787917B2 (en) 2018-05-04 2020-09-29 Rolls-Royce North American Technologies Inc. Multi-piece turbine disk for ceramic matrix composite components
US10934863B2 (en) * 2018-11-13 2021-03-02 Rolls-Royce Corporation Turbine wheel assembly with circumferential blade attachment
US11371351B2 (en) 2020-01-17 2022-06-28 Raytheon Technologies Corporation Multi-disk bladed rotor assembly for rotational equipment
US11286781B2 (en) * 2020-01-17 2022-03-29 Raytheon Technologies Corporation Multi-disk bladed rotor assembly for rotational equipment
US11208892B2 (en) * 2020-01-17 2021-12-28 Raytheon Technologies Corporation Rotor assembly with multiple rotor disks
US11339673B2 (en) * 2020-01-17 2022-05-24 Raytheon Technologies Corporation Rotor assembly with internal vanes
US11401814B2 (en) 2020-01-17 2022-08-02 Raytheon Technologies Corporation Rotor assembly with internal vanes
IT202100029963A1 (it) * 2021-11-26 2023-05-26 Ge Avio Srl Motore a turbina a gas comprendente un complesso di pale rotanti.

Family Cites Families (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1318091A (en) * 1919-10-07 Hredrik ljtjngstrsm
US840310A (en) * 1906-05-14 1907-01-01 Richard H Goldsborough Turbine.
AT74422B (de) * 1913-05-31 1918-07-10 Ver Dampfturbinen Ges Mit Besc Nachgiebige Lagerung von gegeneinander abgestützten, umlaufenden Maschinenteilen. z. B. Turbinenlaufrädern, auf der Welle zum Ausgleich verschiedener Wärmeausdehnung.
CH234848A (de) * 1943-02-09 1944-10-31 Tech Studien Ag Läufer für Kreiselmaschinen mit axial nebeneinander angeordneten, durch Schrauben miteinander verbundenen Drehkörpern.
GB588393A (en) * 1945-02-15 1947-05-21 Frank Felix Evennett Improved joining means for pre-formed walls
US2657008A (en) * 1947-08-07 1953-10-27 Atkinson Joseph Turbine or like rotor
US2539730A (en) * 1947-11-10 1951-01-30 Jeumont Forges Const Elec Composite rim and method of manufacturing the same
US2641440A (en) * 1947-11-18 1953-06-09 Chrysler Corp Turbine blade with cooling means and carrier therefor
US2773169A (en) * 1951-02-26 1956-12-04 Power Jets Res & Dev Ltd Welding of bladed rotors for turbines, compressors, etc.
US2825124A (en) * 1952-02-05 1958-03-04 Gen Motors Corp Method of making a fabricated rotor
US2719438A (en) * 1952-11-22 1955-10-04 Paul J Schiefer Engine flywheel
US2918252A (en) * 1954-12-24 1959-12-22 Rolls Royce Turbine rotor disc structure
DE1144537B (de) * 1960-07-13 1963-02-28 Henschel Werke Ag Anordnung zur Kuehlung der Laufraeder und Beschaufelungen von Turbomaschinen, insbesondere Gasturbinen
US3108782A (en) * 1961-03-30 1963-10-29 American Can Co Turbine wheel and method of manufacture
US3282498A (en) * 1963-06-10 1966-11-01 Lloyd B Smith Construction for high gravity centrifuges and the like
US3357082A (en) * 1963-02-13 1967-12-12 Whiton Machine Company Method of making a turbine wheel
US3253842A (en) * 1963-12-10 1966-05-31 Thiokol Chemical Corp Shear key joint
US3282561A (en) * 1964-12-14 1966-11-01 Associated Electric Ind Ltd Turbine rotors
US3368424A (en) * 1966-06-20 1968-02-13 Richfield Ind Equipment Ltd Flywheels
US3429700A (en) * 1966-09-20 1969-02-25 Teleflex Inc Method of producing composite metal articles by uniting two identical shapes
US3356339A (en) * 1966-12-12 1967-12-05 Gen Motors Corp Turbine rotor
US3662619A (en) * 1970-08-26 1972-05-16 Gen Electric Fail-safe rotary machine
US3880267A (en) * 1973-02-12 1975-04-29 Gleason Works Coupling device having means for relieving circumferential stresses
GB1432875A (en) * 1973-07-11 1976-04-22 Rolls Royce Gas rotor assemblies
US3916495A (en) * 1974-02-25 1975-11-04 Gen Electric Method and means for balancing a gas turbine engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0521614A2 (fr) * 1991-06-06 1993-01-07 General Electric Company Assemblage de disques multiples de rotor
EP0521614A3 (en) * 1991-06-06 1993-02-03 General Electric Company Multiple rotor disk assembly

Also Published As

Publication number Publication date
CA1045041A (fr) 1978-12-26
US4097194A (en) 1978-06-27
JPS52129812A (en) 1977-10-31
DE2712115A1 (de) 1977-10-06

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Legal Events

Date Code Title Description
ST Notification of lapse